SAE AS 5725B-2015 Interface Standard Miniature Mission Store Interface.pdf

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1、_SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising theref

2、rom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2015 SAE InternationalAll rights reserved. No part of this publi

3、cation may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE.TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)Tel: +1 724-776-4970 (out

4、side USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AS5725BAEROSPACESTANDARDAS5725 REV. BIssued 2008-01Revised 2015-12Superseding AS5725AInterfac

5、e Standard, Miniature Mission Store InterfaceRATIONALEThis standard was developed by SAE International. It defines implementation requirements for the electrical interface between platforms and miniature stores, and/or miniature store launch/carriage systems and miniature stores. This document was r

6、evised to incorporate editorial and technical comments received and coordinated by SAE AS-1B2 Aircraft/Store Interface Standards User Group. The changes include items that came out of the validation document development effort and the official release of the connector insert in MIL-STD-1560.TABLE OF

7、 CONTENTS1. SCOPE 4 1.1 Scope 4 1.2 Purpose. 4 1.3 Application. 4 2. APPLICABLE DOCUMENTS 4 2.1 General 4 2.2 Non-Government Publications 4 2.2.1 SAE Publications. 5 2.2.2 ANSI Accredited Publications 5 2.3 U.S. Government Documents . 5 2.3.1 Specifications, Standards, and Handbooks 5 2.4 Order of P

8、recedence. 5 3. DEFINITIONS . 6 4. GENERAL REQUIREMENTS . 9 4.1 System Configurations and Interface Nomenclature. 9 4.2 Interface Signal Set and Classes 10 4.2.1 High Bandwidth (HB) Interface 10 4.2.2 Digital Data Interfaces. 12 4.2.3 Store Mated Interface 12 4.2.4 Carriage Mated Interface 12 4.2.5

9、Safety Enable Discrete Interface. 12 4.2.6 Power Interfaces . 12 4.2.7 Structure Ground Interface 13 4.2.8 Platform Class Interface 13 4.2.9 Physical Interconnection Interface 13 SAE INTERNATIONAL AS5725B Page 2 of 535. DETAILED REQUIREMENTS. 13 5.1 Carriage System Requirements 13 5.1.1 Carriage Sys

10、tem: High Bandwidth (HB) Interface. 13 5.1.2 Carriage System: Digital Data 1 Interface. 15 5.1.3 Carriage System: Fibre Channel Interface 16 5.1.4 Carriage System: Store Mated 16 5.1.5 Carriage System: Carriage Mated Interface 16 5.1.6 Carriage System: Safety Enable Discrete Interface 17 5.1.7 Carri

11、age System: Power Interfaces 18 5.1.8 Carriage System: Structure Ground Interface. 24 5.1.9 Carriage System: Platform Class 24 5.2 Miniature Mission Store Requirements (Measured at the MMSI) . 24 5.2.1 Store: High Bandwidth Interface 24 5.2.2 Store: Digital Data 1 Interface . 26 5.2.3 Store: Fibre C

12、hannel Interface 27 5.2.4 Store: Store Mated Interface . 27 5.2.5 Store: Carriage Mated Interface 27 5.2.6 Store: Safety Enable Discrete Interface 28 5.2.7 Store: Power Interfaces. 29 5.2.8 Store: Structure Ground Interface. 32 5.2.9 Store: Platform Class Interface . 32 5.3 Interface Initialization.

13、 33 5.3.1 Carriage System Initialization Requirements 33 5.3.2 Store Initialization Requirements. 34 5.4 Power Interface Interrupts. 35 5.4.1 Store Compatibility 35 5.4.2 Carriage System Compatibility 35 5.4.3 Store Power Interrupt Notification . 35 5.5 Connector Characteristics. 35 5.5.1 MSCI Conne

14、ctors 35 5.5.2 MMSI Connectors 35 5.5.3 Contacts 36 5.5.4 Connector Insert Arrangement 36 5.5.5 Plugged Cavities . 37 5.5.6 Connector Location and Orientation 37 6. NOTES 37 6.1 Intended Use. 37 6.2 Acquisition Requirements . 37 6.3 Revision Indicator 38 APPENDIX A ADDITIONAL HIGH BANDWIDTH TYPE A S

15、IGNAL PATH REQUIREMENTS FOR MIL-STD-1760MINIATURE STORE CARRIAGE SYSTEMS39APPENDIX B MMSI TO JMMI CROSS REFERENCE 49 APPENDIX C PARTIAL INITIALIZATION REQUEST . 51 FIGURE 1 OVERALL SYSTEM INTERFACE ARRANGEMENT .9 FIGURE 2 SUBPACK CARRIAGE ARRANGEMENT 10 FIGURE 3 INTERFACE SIGNAL SET 11 FIGURE 4A EQU

16、IVALENT CIRCUIT OF MSCI TYPE A INTERFACE (MMSI IS SIGNAL SOURCE). 14 FIGURE 4B EQUIVALENT CIRCUIT OF MSCI HB TYPE A INTERFACE (HOST PLATFORM IS SIGNAL SOURCE) 14 FIGURE 4 EQUIVALENT CIRCUITS OF MSCI HB TYPE A INTERFACES 14 FIGURE 5A EQUIVALENT CIRCUIT OF MSCI HB TYPE B INTERFACE (MMSI IS SIGNAL SOUR

17、CE). 15 FIGURE 5B EQUIVALENT CIRCUIT OF MSCI HB TYPE B INTERFACE (HOST PLATFORM IS SIGNAL SOURCE) 15 FIGURE 5 EQUIVALENT CIRCUITS OF MSCI TYPE B INTERFACES 15 FIGURE 6 OPERATING POWER INTERFACE CURRENT LEVEL 19 FIGURE 7 STABILIZATION TIME 20 FIGURE 8 SAFETY ENABLE POWER INTERFACE CURRENT LEVEL 21 FI

18、GURE 9 AUXILIARY POWER INTERFACE CURRENT LEVEL 23 SAE INTERNATIONAL AS5725B Page 3 of 53FIGURE 10A EQUIVALENT CIRCUIT OF MMSI HB TYPE A INTERFACE (MMSI IS SIGNAL SINK) . 25 FIGURE 10B EQUIVALENT CIRCUIT OF MMSI HB TYPE A INTERFACE (MMSI IS SIGNAL SOURCE) 25 FIGURE 10 EQUIVALENT CIRCUITS OF MMSI HB T

19、YPE A INTERFACES . 25 FIGURE 11A EQUIVALENT CIRCUIT OF MMSI HB TYPE B INTERFACE (MMSI IS SIGNAL SINK) . 26 FIGURE 11B EQUIVALENT CIRCUIT OF MMSI HB TYPE B INTERFACE (MMSI IS SIGNAL SOURCE) 26 FIGURE 11 EQUIVALENT CIRCUITS OF MMSI HB TYPE B INTERFACES . 26 FIGURE 12 CONNECTOR INSERT ARRANGEMENT (15-2

20、1) . 36 TABLE 1 CONNECTOR CONTACTS/TERMINI AND SEAL PLUGS 36 TABLE 2 CONNECTOR CONTACT FUNCTIONAL ASSIGNMENT . 37 SAE INTERNATIONAL AS5725B Page 4 of 531. SCOPE1.1 ScopeThis standard defines implementation requirements for the electrical interface between: a. aircraft carried miniature store carriag

21、e systems and miniature storesb. aircraft parent carriage and miniature storesc. surface based launch systems and miniature storesThe interface provides a common interfacing capability for the initialization and employment of smart miniature munitions and other miniature stores from the host systems

22、. Physical, electrical, and logical (functional) aspects of the interface are addressed.1.2 PurposeThe purpose of this standard is to minimize proliferation of electrical interfaces between platforms, miniature stores and associated carriage systems and thereby promote interoperability of miniature

23、stores and carriage systems across different programs and services.1.3 ApplicationThis standard applies to all platforms, miniature stores and associated carriage systems that electrically interface with each other. The carriage systems include captive and releasable (canister type) aircraft mounted

24、 carriage devices, platforms such as unmanned combat air vehicles (parent carriage), dedicated carriage areas on aircraft, and surface based launch systems. For simplicity within this document, all carrying devices are generically referred to as the miniature store carriage system (or simply carriag

25、e system) from an interface perspective. Additionally, the term store as used in this document refers to a miniature store unless otherwise indicated.2. APPLICABLE DOCUMENTSThe following publications form a part of this document to the extent specified herein. The latest issue of SAE publications sh

26、all apply. The applicable issue of the other publications shall be the issue in effect on the date of the purchase order. Inthe event of conflict between the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes a

27、pplicable laws and regulations unless a specific exemption has been obtained.2.1 GeneralThe documents listed in this section are specified in Sections 3, 4, and 5 of this standard. This section does not include documents cited in other sections of this standard or recommended for additional informat

28、ion or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements documents cited in Sections 3, 4, and 5 of this standard, whether or not they are listed.2.2 Non-Government PublicationsThe follow

29、ing documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of the documents are those cited in the solicitation or contract.SAE INTERNATIONAL AS5725B Page 5 of 532.2.1 SAE PublicationsAvailable from SAE International, 400 Commonwealth Drive, War

30、rendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org.AS5652 10 Megabit/sec Network Configuration Digital Time Division Command/Response Multiplex Data BusAS5653 High Speed Network for MIL-STD-1760AS39029 Contacts, Electrical Connector, Gener

31、al Specification ForAS85049/80 Connector Accessories, Electrical, Dummy Contact, Sizes 16, 12 and 8, Category 7 (For MIL-DTL-38999Connectors)2.2.2 ANSI Accredited PublicationsCopies of these documents are available online at http:/webstore.ansi.org/FC-PI ANSI INCITS 352-2002 Fibre Channel - Physical

32、 interfaces2.3 U.S. Government DocumentsCopies of these documents are available online at http:/quicksearch.dla.mil.2.3.1 Specifications, Standards, and HandbooksThe following specifications, standards, and handbooks form a part of this document to the extent specified herein.STANAG 4294 (Part 1) Na

33、vstar Global Positioning System (GPS) System CharacteristicsMIL-DTL-38999 Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect (Bayonet, Threaded, and Breech Coupling), Environment Resistant, Removable Crimp and Hermetic Solder Contacts, General Specification ForMS27488 Plug,

34、End Seal, Electrical ConnectorMIL-STD-704 Aircraft Electric Power CharacteristicsMIL-STD-1760 Aircraft/Store Electrical Interconnection SystemMIL-STD-1560 Insert Arrangements for MIL-DTL-38999, MIL-DTL-27599, and SAE-as29600 Series A Electrical Circular Connectors2.4 Order of PrecedenceIn the event

35、of a conflict between the text of this document and the references cited herein, the text of this document takesprecedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.SAE INTERNATIONAL AS5725B Page 6 of 533. DEFINITIONS

36、3.1 DefinitionsDefinitions applicable to this standard are as follows.3.1.1 AIRCRAFTAny vehicle designed to be supported by air, being borne up either by the dynamic action of the air upon the surfaces of the vehicle, or by its own buoyancy. The term includes fixed and movable wing airplanes, helico

37、pters, gliders, and airships, but excludes air-launched missiles, target drones, and flying bombs.3.1.2 ELECTRICAL INTERFACE TYPESThe two electrical interface types for the carriage system/store electrical interconnection system shall be as specified below.3.1.2.1 MINIATURE STORE CARRIAGE INTERFACE

38、(MSCI)The electrical interface on the miniature store carriage system structure where the miniature mission store is electrically connected either directly (blind mate) or via an interconnecting umbilical cable.3.1.2.2 MINIATURE MISSION STORE INTERFACE (MMSI)The electrical interface on the miniature

39、 mission store external structure or interconnecting umbilical cable that mates withan MSCI interface on the carriage system.3.1.3 MINIATURE STORE CARRIAGE SYSTEMA system which provides for carriage and release of and electrical interfacing to miniature munitions or other stores that are compliant w

40、ith the miniature store electrical interface standard defined in this document. The miniature store carriage system may be located external to the aircraft in a separate enclosure (possibly releasable) which is electrically interfacedto the aircraft via a MIL-STD-1760 compatible interface, or may be

41、 integrally contained within the structure of an unmanned or manned aircraft platform, or may be included in surface based launch systems. The miniature store carriage system is typically referred to simply as the carriage system in this document.3.1.4 STOREAny device intended for internal or extern

42、al carriage and mounted (either directly or through an intermediary carriage device) on aircraft suspension and release equipment, whether or not the item is intended to be separated in flight from the aircraft. Stores relevant to this standard are miniature stores classified in two categories as sp

43、ecified below. (Note that the generic term store is typically used to refer to miniature stores in this document when the distinction of category is notimportant.)3.1.4.1 MINIATURE MISSION STOREA small munition or other store with an MMSI carried at a station on a miniature store carriage system.3.1

44、.4.2 SUBPACKAn in-flight separable physical package which contains multiple miniature mission stores intended for release as a single entity (for aerodynamic purposes, etc.) from a carriage system. Subpacks provide individual external MMSIs for each carried miniature mission store. A separate extern

45、al MMSI may additionally be provided (as required) on each subpack for interfacing to internal subpack electronics.SAE INTERNATIONAL AS5725B Page 7 of 533.1.5 STORES MANAGEMENT SYSTEMThe avionics subsystem which controls and monitors the operational state of aircraft installed stores and provides an

46、d manages the communications between aircraft stores and other aircraft subsystems.3.1.6 SUSPENSION AND RELEASE EQUIPMENTAll airborne devices used for carriage, suspension, employment, and jettison of stores, such as, but not limited to, racks, adapters, launchers, and pylons.3.1.7 DELAYSignal or da

47、ta delay is the elapsed time between the input stimulus and output response of a particular signal or data path.3.1.8 POWER INTERRUPTIONAn excursion of supplied interface power below the specified normal steady state limits established by this standard.3.1.9 L1_P(Y) SignalThe L1_P(Y) signal is the G

48、PS L1p carrier component of L1, bi-phase shift key (BPSK) modulated by the P(Y) code plus data bit stream, as described in STANAG 4294.3.1.10 L2_P(Y) SignalThe L2_P(Y) signal is the GPS L2p carrier component of L2, bi-phase shift key (BPSK) modulated by the P(Y) code plus data bit stream, as describ

49、ed in STANAG 4294.3.1.11 L1_C/A SignalThe L1_C/A signal is the GPS L1c carrier component of L1, bi-phase shift key (BPSK) modulated by the C/A code plus data bit stream, as described in STANAG 4294.3.1.12 FIBRE CHANNELFibre Channel is the name for a high-speed network standard. Fibre Channel allows for both copper and fiber optic implementations.3.1.13 SAFETY CRITICALAn interface operation (electrical, logical or a combination of both) at